Browse Standards AMS4416B
Current REVISED 2017-05-30

Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged AMS4416B

This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness (see 8.5).
AMS4416B
2017-05-30
Latest
Revised
AMS4416A
2012-10-03
Historical
Revised
AMS4416
2008-07-29
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Preview Document Add to Cart
Members save up to 10% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Aluminum Alloy, Plate (7085-T7451) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged

AMS4470C

View Details

STANDARD

Aluminum Alloy, Plate (2098-O) 3.5Cu - 1.1Li - 0.50Mg - 0.40Ag - 0.11Zr Annealed

AMS4327A

View Details

STANDARD

Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

AMS4413B

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X